Implementation and Comparisons of Parallel Implicit Solvers for Hypersonic Flow Computations on Unstructured Meshes
Author:
Affiliation:
1. University of Minnesota, Minneapolis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3547
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5. Data-Parallel Line Relaxation Method for the Navier-Stokes Equations
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